Metal treatment – Compositions – Heat treating
Patent
1980-04-18
1981-10-13
Dean, R.
Metal treatment
Compositions
Heat treating
75141, 75142, 148 3, 148 115A, 148 127A, 148 32, 148 325, 148159, C22F 104, C22C 2116
Patent
active
042946255
ABSTRACT:
A 2000 series aluminum alloy characterized by high strength, very high fatigue resistance, and very high fracture toughness consists essentially of 3.8% to 4.4% copper, 1.2% to 1.8% magnesium, 0.3% to 0.9% manganese, maximums of 0.12% silicon, 0.15% iron, 0.25% zinc, 0.15% titanium, 0.10% chromium, 0.05% of each of any other trace elements present, and a maximum total of such other trace elements of 0.15%, the balance of the alloy being aluminum. It is preferred, especially for plate products, that the maximum iron and silicon levels be restricted to 0.12% and 0.10%, respectively. For extruded products, the foregoing alloy is hot worked to yield a wrought product having a substantially unrecrystallized structure. For plate products, the alloy is subjected to room temperature preaging and a cold rolling treatment to provide a reduction in gauge of from 9% to 13%.
REFERENCES:
patent: 3826688 (1974-07-01), Levy
Hyatt Michael V.
Quist William E.
Dean R.
The Boeing Company
LandOfFree
Aluminum alloy products and methods does not yet have a rating. At this time, there are no reviews or comments for this patent.
If you have personal experience with Aluminum alloy products and methods, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Aluminum alloy products and methods will most certainly appreciate the feedback.
Profile ID: LFUS-PAI-O-929039